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The JPL advanced propulsion module motor chamberA Kevlar 49/epoxy chamber has been developed for the advanced propulsion module motor. This chamber was successfully designed, fabricated, and hydroproof-tested at 511.6 N/sq cm. The fabrication, interior dimensional inspection, and proof test are discussed, showing that the chamber will be capable of achieving the design burst pressure of 639.8 N/sq cm. The projected chamber growth at 448.2 N/sq cm is presented based on the strain gage and volumetric growth data collected in that proof test.
Document ID
19760055216
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jensen, W. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bailey, R. L. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-637
Meeting Information
Meeting: Propulsion Conference
Location: Palo Alto, CA
Start Date: July 26, 1976
End Date: July 29, 1976
Sponsors: American Institute of Aeronautics and Astronautics and Society of Automotive Engineers
Accession Number
76A38182
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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